BACKGROUND OF THE INVENTION
1. Field of the Invention
Embodiments of the present invention generally relate to a compact cable suspended pumping system for dewatering gas wells.
2. Description of the Related Art
As natural gas wells mature, many experience a decrease in production due to water build up in the annulus creating back pressure on the reservoir. The gas industry have utilized varying technologies to alleviate this problem, however most do not meet the economic hurdle as they require intervention such as pulling the tubing string.
SUMMARY OF THE INVENTION
Embodiments of the present invention generally relate to a compact cable suspended pumping system for dewatering gas wells. In one embodiment, a method of unloading liquid from a reservoir includes deploying a pumping system into a wellbore to a location proximate the reservoir using a cable. The pumping system includes a multi-section motor, an isolation device, and a pump. The method further includes supplying a power signal from the surface to the motor via the cable and sequentially operating each section of the motor to mimic a multi-phase motor, thereby driving the pump and lowering a liquid level in the tubular string to a level proximate the reservoir.
In another embodiment, a pumping system includes a submersible multi-section electric motor operable to rotate a drive shaft. Each section is incrementally oriented so that the sections are operable to mimic a multi-phase motor. The pumping system further includes a pump rotationally connected to the drive shaft; an isolation device operable to engage a tubular string, thereby fluidly isolating an inlet of the pump from an outlet of the pump and rotationally connecting the motor and the pump to the tubular string; and a cable having two or less conductors, a strength sufficient to support the motor, the pump, and the isolation device, and in electrical communication with the motor.
In another embodiment, a motor includes two or more sections. Each section includes a submersible tubular housing and a stator core disposed within the housing. The stator core has one or more lobes and each lobe has a winding wrapped therearound. The motor further includes a rotor disposed within the housing and including a shaft and a rotor core. The rotor core has two or more lobes. Each section is incrementally oriented so that the sections may be operated to mimic a multi-phase motor.
BRIEF DESCRIPTION OF THE DRAWINGS
So that the manner in which the above recited features of the present invention can be understood in detail, a more particular description of the invention, briefly summarized above, may be had by reference to embodiments, some of which are illustrated in the appended drawings. It is to be noted, however, that the appended drawings illustrate only typical embodiments of this invention and are therefore not to be considered limiting of its scope, for the invention may admit to other equally effective embodiments.
FIG. 1A illustrates a pumping system, such as an electric submersible pumping system, deployed in a wellbore, according to one embodiment of the present invention. FIG. 1B illustrates an electric submersible pumping system deployed in a wellbore, according to another embodiment of the present invention.
FIG. 2A is a layered view of the power cable. FIG. 2B is an end view of the power cable.
FIG. 3A is an external view of the motor minus the housing. FIG. 3B is an enlargement of a portion of FIG. 3A. FIG. 3C is a schematic of the multi-section motor mimicking operation of a multi-phase motor. FIG. 3D is a cross section of the stator. FIG. 3E is a cross section of the rotor.
FIG. 4A is a cross-section of a stage of the pump. FIG. 4B is an external view of a mandrel of the pump stage.
DETAILED DESCRIPTION
FIG. 1A illustrates a pumping system, such as an electric submersible pumping system (ESP) 1, deployed in a wellbore 5, according to one embodiment of the present invention. The wellbore 5 has been drilled from a surface of the earth 20 or floor of the sea (not shown) into a hydrocarbon-bearing (i.e., natural gas 100 g) reservoir 25. A string of casing 10 c has been run into the wellbore 5 and set therein with cement (not shown). The casing 10 c has been perforated 30 to provide to provide fluid communication between the reservoir 25 and a bore of the casing 10. A wellhead 15 has been mounted on an end of the casing string 10 c. An outlet line 35 extends from the wellhead 15 to production equipment (not shown), such as a separator. A production tubing string 10 t has been run into the wellbore 5 and hung from the wellhead 15. A production packer 85 has been set to isolate an annulus between the tubing 10 t and the casing 10 c from the reservoir 25. The reservoir 25 may be self-producing until a pressure of the gas 100 g is no longer sufficient to transport a liquid, such as water 100 w, to the surface. A level of the water 100 w begins to build in the production tubing 10 t, thereby exerting hydrostatic pressure on the reservoir 25 and diminishing flow of gas 100 g from the reservoir 25.
FIG. 1B illustrates the ESP 1 deployed in a wellbore 5, according to another embodiment of the present invention. In this embodiment, the casing 10 c has been used to produce fluid from the reservoir 25 instead of installing production tubing. In this scenario, the isolation device 70 may be set against the casing 10 c and the pump 65 may discharge the water 100 w to the surface 20 via a bore of the casing 10 c.
The ESP 1 may include a surface controller 45, an electric motor 50, a power conversion module (PCM) 55, a seal section 60, a pump 65, an isolation device 70, a cablehead 75, and a power cable 80. Housings of each of the downhole components 50-75 may be longitudinally and rotationally connected, such as with flanged or threaded connections. The downhole component housings may be made from a corrosion resistant metal or alloy, such as galvanized steel, stainless steel, or a nickel based alloy. Since the downhole components 50-75 may be deployed within the tubing 10 t, the components 50-80 may be compact, such as having a maximum outer diameter less than or equal to two or one and three-quarter inches (depending on the inner diameter of the tubing 10 t).
The surface controller 45 may be in electrical communication with an alternating current (AC) power source 40, such as a generator on a workover rig (not shown). The surface controller 45 may include a transformer (not shown) for stepping the voltage of the AC power signal from the power source 40 to a medium voltage (V) signal. The medium voltage may be greater than or equal to one kV, such as five to ten kV. The surface controller may further include a rectifier for converting the medium voltage AC signal to a medium voltage direct current (DC) power signal for transmission downhole via the power cable 80. The surface controller 45 may further include a data modem (not shown) and a multiplexer (not shown) for modulating and multiplexing a data signal to/from the PCM 55 with the DC power signal. The surface controller 45 may further include an operator interface (not shown), such as a video-display, touch screen, and/or USB port.
The cable 80 may extend from the surface controller 45 through the wellhead 15 or connect to leads which extend through the wellhead 15 and to the surface controller 45. The cable 80 may be received by slips or a clamp (not shown) disposed in or proximate to the wellhead 15 for longitudinally connecting the cable 80 to the wellhead 15 during operation of the ESP 1. The cable 80 may extend into the wellbore 5 to the cablehead 75. Since the power signal may be DC, the cable 80 may only include two conductors arranged coaxially.
FIG. 2A is a layered view of the power cable 80. FIG. 2B is an end view of the power cable 80. The cable 80 may include an inner core 205, an inner jacket 210, a shield 215, an outer jacket 230, and armor 235, 240. The inner core 205 may be the first conductor and made from an electrically conductive material, such as aluminum, copper, aluminum alloy, or copper alloy. The inner core 205 may be solid or stranded. The inner jacket 210 may electrically isolate the core 205 from the shield 215 and be made from a dielectric material, such as a polymer (i.e., an elastomer or thermoplastic). The shield 215 may serve as the second conductor and be made from the electrically conductive material. The shield 215 may be tubular, braided, or a foil covered by a braid. The outer jacket 230 may electrically isolate the shield 215 from the armor 235, 240 and be made from an oil-resistant dielectric material. The armor may be made from one or more layers 235, 240 of high strength material (i.e., tensile strength greater than or equal to two hundred kpsi) to support the deployment weight (weight of the cable and the weight of the downhole components 50-75) so that the cable 80 may be used to deploy and remove the downhole components 50-75 into/from the wellbore 5. The high strength material may be a metal or alloy and corrosion resistant, such as galvanized steel, stainless steel, or a nickel alloy depending on the corrosiveness of the gas 100 g. The armor may include two contra-helically wound layers 235, 240 of wire or strip.
Additionally, the cable 80 may include a sheath 225 disposed between the shield 215 and the outer jacket 230. The sheath 225 may be made from lubricative material, such as polytetrafluoroethylene (PTFE) or lead and may be tape helically wound around the shield 215. If lead is used for the sheath, a layer of bedding 220 may insulate the shield 215 from the sheath and be made from the dielectric material. Additionally, a buffer 245 may be disposed between the armor layers 235, 240. The buffer 245 may be tape and may be made from the lubricative material.
Due to the coaxial arrangement, the cable 80 may have an outer diameter 250 less than or equal to one and one-quarter inches, one inch, or three-quarters of an inch.
Additionally, the cable 80 may further include a pressure containment layer (not shown) made from a material having sufficient strength to contain radial thermal expansion of the dielectric layers and wound to allow longitudinal expansion thereof. The material may be stainless steel and may be strip or wire. Alternatively, the cable 80 may include only one conductor and the tubing 10 t may be used for the other conductor.
The cable 80 may be longitudinally connected to the cablehead 75. The cablehead 75 may also include leads (not shown) extending therethrough. The leads may provide electrical communication between the conductors of the cable 80 and the PCM 55.
FIG. 3A is an external view of the motor 50 minus the housing. FIG. 3B is an enlargement of a portion of FIG. 3A. FIG. 3C is a schematic of the multi-section motor 50 mimicking operation of a multi-phase motor. FIG. 3D is a cross section of the stator 110 s. FIG. 3E is a cross section of the rotor 110 r.
The motor 50 may be filled with a dielectric, thermally conductive liquid lubricant, such as mineral oil. The motor 50 may be cooled by thermal communication with the reservoir water 100 w. The motor 50 may include a thrust bearing (not shown) for supporting a drive shaft 135. In operation, the motor 50 may rotate the shaft 135, thereby driving the pump 65. The motor shaft 135 may be directly (no gearbox) connected to a rotor 160 of the pump via a shaft of the motor seal 60. As discussed above, since the motor 50 may be compact, the motor may operate at high speed so that the pump may generate the necessary head to pump the water 100 w to the surface 20. High speed may be greater than or equal to ten or fifteen thousand revolutions per minute (RPM).
The motor 50 may include two or more sections 105 a-c, 106 a-c. Each section 105 a-c, 106 a-c may include a rotor 110 r and a stator 110 s. The stator 110 s may include the housing 115, a core 120 s, windings 125, and leads 130. The housing 115 may be tubular and have a bore therethrough. Each section 105 a-c, 106 a-c may be longitudinally and rotationally connected, such as by flanges or threads (not shown). The core 120 s may include one or more lobes 121 (two shown). Each lobe 121 may be wound and the windings 125 of opposing lobes 121 may be connected (not shown) in series or parallel to define a phase. The motor 50 may further include one or more sets, such as a first set 105 and a second set 106 (not shown) of sections 105 a-c, 106 a-c. The stator 110 s of each section 105 a-c, 106 a-c of each set 105, 106 may be incrementally oriented relative to each other based on a three-hundred and sixty degree sum. For example, for three sections, each section 105 a-c, 106 a-c may be shifted by one-hundred twenty degrees relative to other sections of the set. Alternatively, each rotor 110 r of each section 105 a-c, 106 a-c of each set 105, 106 may be shifted instead of shifting the stators 110 s.
Each section 105 a-c, 106 a-c may be electrically connected to the PCM 55 by the leads 130. Respective sections (i.e., 105 a, 106 a) of each set 105, 106 may correspond, thereby operating as a single phase. The corresponding sections of the sets 105, 106 may be electrically connected to the PCM 55 in parallel or series. Shifted sections (i.e., 105 a, b) of each set 105, 106 may be connected to the PCM 55 in parallel. Each set 105, 106 may be controlled by the PCM 55 to mimic one or more multi-phase motors 105 e (may be viewed as a single motor or two motors in series), such as a three-phase (six stator lobes) motor. Other than for the orientation, each of the sections 105 a-c, 106 a-c may be identical, thereby forming a modular motor 50.
The motor 50 may be a switched reluctance motor (SRM). Each rotor 110 r may include a shaft 135 and a core 120 r. The shaft 135 may be made from a metal or alloy, such as plain carbon or low alloy steel, stainless steel, or a nickel based alloy. The core 120 r may have two or more lobes 122, such as four, each spaced apart by ninety degree increments. Each of the cores 120 s, 120 r may be laminates. Each layer of the laminates may be made from a metal or alloy, such as silicon steel. The layers may be aligned and then pressed together to form one of the cores 120 r,s. The windings 125 may then be wrapped around each lobe 121. The stator core 120 s may be longitudinally and rotationally connected to the housing 115, such as by a key and keyway (not shown) and fasteners. The housing 115 may include an external indicator (not shown), such as a groove or protrusion, to facilitate orientation of the sections 105 a-c, 106 a-c with respect to one another. The rotor core 120 r may be longitudinally and rotationally connected to the shaft 135, such as by a key, keyway, and fasteners or an interference fit. Each of the leads 130 and windings 125 may include a core made from an electrically conductive material, as discussed above, and be jacketed by a dielectric material, as discussed above.
Each section 105 a-c, 106 a-c may further include a bearing 140, such as a radial bearing, for supporting rotation of the shaft 135 relative to the housing 115. The bearing 140 may be a rolling element bearing, such as a ball bearing. The bearing 140 may include a gland 141 housing an outer race 142 s. The gland 141 may be connected (not shown) to the housing 115 and the outer race 142 s connected to the gland 141. The bearing 140 may further include an inner race 142 r connected to the shaft 135. Balls 143 (schematically shown) may be disposed between the races 142 r,s and lubricant may be sealed within the races. Alternatively, the bearing 140 may be a hydrodynamic bearing, as discussed below.
The PCM 55 may include a motor controller (not shown), a modem (not shown), and demultiplexer (not shown). The modem and demultiplexer may demultiplex a data signal from the DC power signal, demodulate the signal, and transmit the data signal to the motor controller. The motor controller may receive the medium voltage DC signal from the cable and sequentially energize the shifted sections 105 a-c (& 106 a-c) of the motor 50, thereby supplying an output signal to drive the particular section of the motor and coordinating operation of each set of sections as a multi-phase motor. The output signal may be stepped, trapezoidal, or sinusoidal. The motor controller may include a logic circuit for simple control (i.e. predetermined speed) or a microprocessor for complex control (i.e., variable speed drive and/or soft start capability). The motor controller may use one or two-phase excitation, be unipolar or bi-polar, and control the speed of the motor by controlling the switching frequency. The motor controller may include an asymmetric bridge or half-bridge.
Alternatively, the motor 50 may be permanent magnet motor, such as a brushless DC motor (BLDC) made in a similar multi-section fashion. The BLDC motor may include three shifted stator sections to mimic a three phase (two pole) winding, a permanent magnet rotor, and a rotor position sensor. The permanent magnet rotor may be made of a rare earth magnet or a ceramic magnet. The rotor position sensor may be a Hall-effect sensor, a rotary encoder, or sensorless (i.e., measurement of back EMF in undriven coils by the motor controller). The BLDC motor controller may be in communication with the rotor position sensor and include a bank of transistors or thyristors and a chopper drive for complex control (i.e., variable speed drive and/or soft start capability).
Additionally, the PCM 55 may include a power supply (not shown). The power supply may include one or more DC/DC converters, each converter including an inverter, a transformer, and a rectifier for converting the DC power signal into an AC power signal and stepping the voltage from medium to low, such as less than or equal to one kV. The power supply may include multiple DC/DC converters in series to gradually step the DC voltage from medium to low. The low voltage DC signal may then be supplied to the motor controller.
The motor controller may be in data communication with one or more sensors (not shown) distributed throughout the downhole components 50-75. A pressure and temperature (PT) sensor may be in fluid communication with the water 100 w entering the intake 65 i. A gas to liquid ratio (GLR) sensor may be in fluid communication with the water 100 w entering the intake 65 i. A second PT sensor may be in fluid communication with the water 100 w discharged from the outlet 65 o. A temperature sensor (or PT sensor) may be in fluid communication with the lubricant to ensure that the motor and downhole controller are being sufficiently cooled. Multiple temperature sensors may be included in the PCM 55 for monitoring and recording temperatures of the various electronic components. A voltage meter and current (VAMP) sensor may be in electrical communication with the cable 80 to monitor power loss from the cable. A second VAMP sensor may be in electrical communication with the motor controller output to monitor performance of the motor controller. Further, one or more vibration sensors may monitor operation of the motor 50, the pump 65, and/or the seal section 60. A flow meter may be in fluid communication with the discharge 65 o for monitoring a flow rate of the pump 65. Utilizing data from the sensors, the motor controller may monitor for adverse conditions, such as pump-off, gas lock, or abnormal power performance and take remedial action before damage to the pump 65 and/or motor 50 occurs.
The seal section 60 may isolate the water 100 w being pumped through the pump 65 from the lubricant in the motor 50 by equalizing the lubricant pressure with the pressure of the water 100 w. The seal section 60 may rotationally connect the motor shaft 135 to a drive shaft of the pump 65. The shaft seal may house a thrust bearing capable of supporting thrust load from the pump 65. The seal section 60 may be positive type or labyrinth type. The positive type may include an elastic, fluid-barrier bag to allow for thermal expansion of the motor lubricant during operation. The labyrinth type may include tube paths extending between a lubricant chamber and a water chamber providing limited fluid communication between the chambers.
The pump may include an inlet 65 i. The inlet 65 i may be standard type, static gas separator type, or rotary gas separator type depending on the GLR of the reservoir fluid. The standard type intake may include a plurality of ports allowing water 100 w to enter a lower or first stage of the pump 65. The standard intake may include a screen to filter particulates from the water 100 w. The static gas separator type may include a reverse-flow path to separate a gas portion of the reservoir fluid from a liquid portion of the reservoir fluid.
FIG. 4A is a cross-section of a stage 65 s of the pump 65. FIG. 4B is an external view of a mandrel 155 of the pump stage 65 s. The pump 65 may include one or more stages 65 s, such as six. Each stage 65 s may be longitudinally and rotationally connected, such as with threaded couplings or flanges (not shown). Each stage 65 s may include a housing 150, a mandrel 155, and an annular passage 170 formed between the housing and the mandrel. The housing 150 may be tubular and have a bore therethrough. The mandrel 155 may be disposed in the housing 150. The mandrel 155 may include a rotor 160, one or more helicoidal rotor vanes 160 a,b, a diffuser 165, and one or more diffuser vanes 165 v. The rotor 160, housing 155, and diffuser 165 may each be made from a metal, alloy, or cermet corrosion and erosion resistant to the production fluid, such as steel, stainless steel, or a specialty alloy, such as chrome-nickel-molybdenum. Alternatively, the rotor, housing, and diffuser may be surface-hardened or coated to resist erosion.
The rotor 160 may include a shaft portion 160 s and an impeller portion 160 i. The portions 160 i,s may be integrally formed. Alternatively, the portions 160 i,s may be separately formed and longitudinally and rotationally connected, such as by a threaded connection. The rotor 160 may be supported from the diffuser 165 for rotation relative to the diffuser and the housing 150 by a hydrodynamic radial bearing (not shown) formed between an inner surface of the diffuser and an outer surface of the shaft portion 160 s. The radial bearing may utilize production fluid or may be isolated from the production fluid by one or more dynamic seals, such as mechanical seals, controlled gap seals, or labyrinth seals. The diffuser 165 may be solid or hollow. If the diffuser is hollow, it may serve as a lubricant reservoir in fluid communication with the hydrodynamic bearing. Alternatively, one or more rolling element bearings, such as ball bearings (see bearing 140, discussed above), may be disposed between the diffuser 165 and shaft portion 160 s instead of the hydrodynamic bearings.
The rotor vanes 160 a,b may be formed with the rotor 160 and extend from an outer surface thereof or be disposed along and around an outer surface thereof. Alternatively the rotor vanes 160 a,b may be deposited on an outer surface of the rotor after the rotor is formed, such as by spraying or weld-forming. The rotor vanes 160 a,b may interweave to form a pumping cavity therebetween. A pitch of the pumping cavity may increase from an inlet 170 i of the stage 65 s to an outlet 170 o of the stage. The rotor 160 may be longitudinally and rotationally coupled to the motor drive shaft and be rotated by operation of the motor. As the rotor is rotated, the water 100 w may be pumped along the cavity from the inlet 170 i toward the outlet 170 o.
An outer diameter of the impeller 160 i may increase from the inlet 170 i toward the outlet 170 o in a curved fashion until the impeller outer diameter corresponds to an outer diameter of the diffuser 165. An inner diameter of the housing 150 facing the impeller portion 160 i may increase from the inlet 170 i to the outlet 170 o and the housing inner surface may converge toward the impeller outer surface, thereby decreasing an area of the passage 170 and forming a nozzle 170 n. As the water 100 w is forced through the nozzle 170 n by the rotor vanes 160 a,b, a velocity of the water 100 w may be increased.
The stator may include the housing 150 and the diffuser 165. The diffuser 165 may be formed integrally with or separately from the housing 150. The diffuser 165 may be tubular and have a bore therethrough. The rotor 160 may have a shoulder between the impeller 160 i and shaft 160 s portions facing an end of the diffuser 165. The shaft portion 160 s may extend through the diffuser 165. The diffuser 165 may be longitudinally and rotationally connected to the housing 150 by one or more ribs. An outer diameter of the diffuser 165 and an inner diameter of the housing 150 may remain constant, thereby forming a throat 170 t of the passage 170. The diffuser vanes 165 v may be formed with the diffuser 165 and extend from an outer surface thereof or be disposed along and around an outer surface thereof. Alternatively the diffuser vanes 165 v may be deposited on an outer surface of the diffuser after the diffuser is formed, such as by spraying or weld-forming. Each diffuser vane 165 v may extend along an outer surface of the diffuser 165 and curve around a substantial portion of the circumference thereof. Cumulatively, the diffuser vanes 165 v may extend around the entire circumference of the diffuser 165. The diffuser vanes 165 v may be oriented to negate swirl in the flow of water 100 w caused by the rotor vanes 160 a,b, thereby minimizing energy loss due to turbulent flow of the water 100 w. In other words, the diffuser vanes 165 v may serve as a vortex breaker. Alternatively, a single helical diffuser vane may be used instead of a plurality of diffuser vanes 165 v.
An outer diameter of the diffuser 165 may decrease away from the inlet 170 i to the outlet 170 o in a curved fashion until an end of the diffuser 165 is reached and an outer surface of the shaft portion 160 s is exposed to the passage 170. An inner diameter of the housing 150 facing the diffuser 165 may decrease away from the inlet 170 i to the outlet 170 o and the housing inner surface may diverge from the diffuser outer surface, thereby increasing an area of the passage 170 and forming a diffuser 170 d. As the water 100 w flows through the diffuser 170 d, a velocity of the water 100 w may be decreased. Inclusion of the Venturi 170 n,t,d may also minimize fluid energy loss in the water discharged from the rotor vanes 160 a,b.
As discussed above, for compactness, the motor 50 and pump 65 may operate at the high speed so that the compact pump 65 may generate the necessary head to pump the water 100 w to the outlet line 35 while minimizing a diameter thereof.
The isolation device 70 may include a packer, an anchor, and an actuator. The actuator may include a brake, a cam, and a cam follower. The packer may be made from a polymer, such as a thermoplastic or elastomer, such as rubber, polyurethane, or PTFE. The cam may have a profile, such as a J-slot and the cam follower may include a pin engaged with the J-slot. The anchor may include one or more sets of slips, and one or more respective cones. The slips may engage the production tubing 10 t, thereby rotationally connecting the downhole components 50-75 to the production tubing. The slips may also longitudinally support the downhole components 50-75. The brake and the cam follower may be longitudinally connected and may also be rotationally connected. The brake may engage the production tubing 10 t as the downhole components 50-75 are being run-into the wellbore. The brake may include bow springs for engaging the production tubing. Once the downhole components 50-75 have reached deployment depth, the cable 80 may be raised, thereby causing the cam follower to shift from a run-in position to a deployment position. The cable 80 may then be relaxed, thereby, causing the weight of the downhole components 50-75 to compress the packer and the slips and the respective cones, thereby engaging the packer and the slips with the production tubing 10 t. The isolation device 70 may then be released by pulling on the cable 80, thereby again shifting the cam follower to a release position. Continued pulling on the cable 80 may release the packer and the slips, thereby freeing the downhole components 50-75 from the production tubing 10 t.
Alternatively, the actuator may include a piston and a control valve. Once the downhole components 50-75 have reached deployment depth, the motor 50 and pump 65 may be activated. The control valve may remain closed until the pump exerts a predetermined pressure on the valve. The predetermined pressure may cause the piston to compress the packer and the slips and cones, thereby engaging the packer and the slips with the production tubing. The valve may further include a vent to release pressure from the piston once pumping has ceased, thereby freeing the slips and the packer from the production tubing. Additionally, the actuator may further be configured so that relaxation of the cable 80 also exerts weight to further compress the packer, slips, and cones and release of the slips may further include exerting tension on the cable 80.
Additionally, the isolation device 70 may include a bypass vent (not shown) for releasing gas separated by the inlet 65 i that may collect below the isolation device and preventing gas lock of the pump 65. A pressure relief valve (not shown) may be disposed in the bypass vent. Additionally, a downhole tractor (not shown) may be integrated into the cable 80 to facilitate the delivery of the downhole components 50-75, especially for highly deviated wells, such as those having an inclination of more than forty-five degrees or dogleg severity in excess of five degrees per one hundred feet. The drive and wheels of the tractor may be collapsed against the cable and deployed when required by a signal from the surface.
In operation, to install the ESP 1, a workover rig (not shown) and the ESP 1 may be deployed to the wellsite. Since the cable 80 may include only two conductors, the cable 80 may be delivered wound onto a drum (not shown). The wellhead 15 may be opened. The components 50-75 may be suspended over the wellbore 5 from the workover rig and an end of the cable 80 may be connected to the cablehead 75. The cable 80 may be unwound from the drum, thereby lowering the downhole components 50-75 into the wellbore 5 inside of the production tubing 10 t. Once the downhole components 50-75 have reached the desired depth proximate to the reservoir 25, the wellhead 15 may be closed and the conductors of the cable 80 may be connected to the surface controller 45.
The isolation device 70 may then be set. Once the isolation device 70 is set, the motor 50 may then be started (if not already started to set the isolation device). If the motor controller is variable, the motor controller may soft start the motor 50. As the pump 65 is operating, the motor controller may send data from the sensors to the surface so that the operator may monitor performance of the pump. If the motor controller is variable, a speed of the motor 50 may be adjusted to optimize performance of the pump 65. Alternatively, the surface operator may instruct the motor controller to vary operation of the motor. The pump 65 may pump the water 100 w through the production tubing 10 t and the wellhead 15 into the outlet 35, thereby lowering a level of the water 100 w and reducing hydrostatic pressure of the water 100 w on the formation 25. The pump 65 may be operated until the water level is lowered to the inlet 65 i of the pump, thereby allowing natural production from the reservoir 25. The operator may then send instructions to the motor controller to shut down the pump 65 or simply cut power to the cable 80. The isolation device 70 may then be unset (if not unset by shutdown of the pump) by winding the drum to exert sufficient tension in the cable 80. The cable 80 may be wound, thereby raising the downhole components 50-75 from the wellbore 5. The workover rig and the ESP 1 may then be redeployed to another wellsite.
Advantageously, deployment of the downhole components 50-75 using the cable 80 inside of the production tubing 10 t instead of removing the production tubing string and redeploying the production tubing string with a permanently mounted artificial lift system reduces the required size of the workover rig and the capital commitment to the well. Deployment and removal of the ESP 1 to/from the wellsite may be accomplished in a matter of hours, thereby allowing multiple wells to be dewatered in a single day. Transmitting a DC power signal through the cable 80 reduces the required diameter of the cable, thereby allowing a longer length of the cable 80 (i.e., five thousand to eight thousand feet) to be spooled onto a drum, and easing deployment of the cable 80.
While the foregoing is directed to embodiments of the present invention, other and further embodiments of the invention may be devised without departing from the basic scope thereof, and the scope thereof is determined by the claims that follow.